Official Projects

A quantitative analysis of mass and surface effects on the burn rate in spherical sugar-based rocket fuel.

This study aims to investigate and clarify the fundamental relationship between the burning surface area of rocket propellants and their mass as well as how this affects the burn rate and mass consumption rate The intention is to fill a knowledge gap within the field of amateur rocketry The goal is to develop a universally applicable model for the burn profile of rocket propellants which can be used in other studies and applications.